AD/HS 125/65 - Main Landing Gear Jack Attachment Bracket - Inspection
1AD/HS 125/65 - Main Landing Gear Jack Attachment Bracket - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/HS 125/65 - Main Landing Gear Jack Attachment Bracket - Inspection.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/65 Main Landing Gear Jack Attachment Bracket - Inspection
7/84
Applicability: All models HS/DH/BH 125 incorporating long range fuel tank (modification 255640). Document: British Aerospace 125 Service Bulletin 32-200.
Compliance: (a) For aircraft with more than 3000 landings as at 31 July 1984 - not later than 30 September 1984.
(b) For aircraft with less than 3000 landings - before exceeding 3000 landings.
Background: Cracking of jack attachment brackets and adjacent door structure has been reported on overseas aircraft. Such cracking could affect opening of the main landing gear doors, thus preventing the gear from lowering.